发明名称 QUIET LANDING ATTITUDE MODIFIER FOR AIRCRAFT
摘要 PROBLEM TO BE SOLVED: To provide a method for adjusting pitching of an aircraft, while overcoming a problem related to noise during landing.SOLUTION: The method includes: commanding flaps to move to a landing setting; providing a current value for a flight condition parameter; providing a current flaps setting; comparing the current value to at least one threshold value; if the current value exceeds the threshold, determining a new flaps setting that can produce an improvement in at least one of a selected aft body contact margin and a selected nose gear contact margin for the aircraft; and adjusting the flaps to the new flaps setting.
申请公布号 JP2013141980(A) 申请公布日期 2013.07.22
申请号 JP20130002645 申请日期 2013.01.10
申请人 BOEING CO:THE 发明人 BUCHHOLZ ROBERT E;EVENS MONTE R;LEE JONATHAN P;OVERTON TIMOTHY G;THOREEN ADAM M
分类号 B64D45/04;B64C13/18 主分类号 B64D45/04
代理机构 代理人
主权项
地址